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Radar Observations
of Solar System Objects
!
Science at (Sometimes)
Negative Redshift
Patrick A. Taylor
!
Arecibo Observatory
!
with lots of help from the radar community
!
8th NAIC/NRAO Single Dish Summer School
July 8, 2015 @ Green Bank, WV
Right: Arecibo!
305m diameter!
1 MW transmitter!
12.6 cm, 2380 MHz!
Fixed dish
Left: Goldstone (DSS-13)!
70m diameter!
500 kW transmitter!
3.5 cm, 8560 MHz!
Steerable dish
Radar Basics
Create an observing
ephemeris that predicts
Doppler shift and range
to the target.!
Generate 2 MW of
power with diesel
generators.!
Output coherent
radiation from klystrons
with ~50% efficiency.
Transmit a polarized signal at a known frequency for a certain time interval.!
Signal bounces off of the target and returns to the telescope. The receiver
is moved into the focus and detects the weak echo in two polarizations.
What is Transmitted?!
We control the signal!
• Continuous Wave: transmit a monochromatic tone
(no frequency, amplitude, or phase modulation)!
!
• Delay-Doppler Ranging/Imaging: !
• Transmit a signal that is phase modulated by a
pseudo-random code!
• The frequency of the phase modulation translates
to resolution in range, e.g., 20 MHz modulation
gives 0.05 us delay resolution or 7.5 range
resolution
What is Received?!
Any Changes are Due to the Object!
• Received signal is very weak: ~10-27 of transmitted
signal returns to the receiver!!
• Signal is mixed, filtered, attenuated, amplified, etc.
and the voltage is recorded as a function of time!
!
• Continuous Wave: Fourier transform the voltage to
get the component frequencies!
• Delay-Doppler Imaging: Cross-correlate the
voltage with the transmitted code to get delay/range
information, then Fourier transform to get frequency
information
Signal-to-Noise Considerations
Want high power, large effective area (gain); !
a big and close target is best
Narrow bandwidths improve SNR
Bandwidth indicates rotation rate!
AND/OR viewing geometry
What Do We Measure?
D = Distance (time delay)
V = Velocity (Doppler shift)
– Orbital D, V!
!
– Object D depth!!
– Object V dispersion
– Scattering properties !
Orbit improvement!
Size and shape!
Spin and shape!
Surface roughness
Observe the Moon, Mercury, Venus, Mars, the Galilean
satellites, Saturn’s rings, near-Earth asteroids,
main-belt asteroids, and comets
Orbit Improvement (Astrometry)
• Radar detects rather than discovers!
• High-precision determination of distance to the target and
line-of-sight velocity!
• Orthogonal to plane-of-sky optical observations!
• Reduce pre-radar orbit uncertainties by five orders of
magnitude for newly discovered objects!
• Extend Earth encounter predictions by factor of five!
• Invaluable for impact hazard assessment!
Left: 2014 YQ8!
!
Right: Bennu
Delay-Doppler Radar Images
• Map a 3D object to a 2D image!
Circles: Represent lines of constant range!
Lines: Represent lines of constant Doppler shift
Doppler shift
range
Blue dots map to same point in delay-Doppler image (N-S ambiguity)
Comparison to Spacecraft
(25143) Itokawa: Hayabusa vs. radar
490 x 310 x 260 m
Radar is a relatively inexpensive method of studying the population
of near-Earth asteroids, capable of reaching fine resolutions only
surpassed by costly, object-specific spacecraft missions.
For Visualizations of asteroid 25143 Itokawa, Radar-Derived
Shape Models, and Their Corresponding Synthetic Radar Spectra
and Radar Images, see Dr. James E. Richardson’s (Arecibo
Observatory) YouTube Channel at:!
https://www.youtube.com/user/jerichardsonjr
Moon
• Delay-Doppler
image mapped to
latitude-longitude!
• 20-m resolution!
• Exceeded only by
recent spacecraft!
• No obvious
evidence for ice at
the south pole!
• High polarization
ratio apparently
due to roughness
Mercury
• Determination of
Mercury’s rotation rate and
the 3:2 spin:orbit
resonance (1965)!
• Determination that
Mercury is in a Cassini
state with a partially
molten core (2007)!
• Detection of radar-bright
material in permanently
shadowed craters,
presumably ice, confirmed
by MESSENGER
Venus
Rotation period also determined by radar
(1964; but not at Arecibo)!
Below: delay-Doppler image!
Right: lat.-lon. map of Maxwell Montes
5 km resolution
1.2 km
Mars: Olympus Mons
Left: 3 km resolution
Above: Viking 1
Mars: Elysium
d
3 km resolution
Saturn
There are two strange things about this image…
Observed Asteroid Population
• Varieties of asteroids observed with radar:!
– Spheroidal!
– Irregular !
– Multiple-component systems!
– Fast rotators (minutes)!
– Slow rotators (days)
MBA (216)
Kleopatra
2006 SX217
1999 JM8
Spheroidal 2005 YU55
• Flew by Earth at 0.85 lunar
distances on November 8, 2011!
• Closest known flyby from a 400-m
scale object in over 30 years!
• Perfect target for Goldstone
(images at left), Arecibo images
below had less resolution
Contact Binaries ~ 1 in 7
2002 NY40
2007 VD12
2005 CR37
(4450) Pan
(11066) Sigurd
1996 HW1
Comet 8P/Tuttle
Columns are Radar Data, Synthetic Data, and Model on Plane of Sky
Comet 103P/Hartley 2
• Used radar to pinpoint the comet’s position and velocity to help Deep
Impact’s navigation team prepare for the 2010 flyby!
• Images reveal a bowling-pin shape with two lobes similar to 8P/Tuttle
Comet 103P/Hartley 2
Nov. 4, 2010 flyby performed by NASA's Deep Impact spacecraft
2014 HQ124
• Approached within 5 lunar distances on
June 8, 2014!
• Too close for Arecibo to resolve in Doppler
frequency!!
• Perfect target for a bistatic experiment!
!
• Goldstone continuously transmits at X
band with 3.5 meter resolution!
• Arecibo continuously receives with no
limitation on the Doppler resolution!
• This configuration is 5x more sensitive
than Goldstone working alone
24
Ultra-rapid Rotators
• 2006 AM4!
– diameter of 150 m!
– 5 minute rotation!!
• 2015 HM10!
– 80 x 40 m in diameter!
– 22 minute rotation!
!
!
• Any loose surface material must be lost!
Binaries Everywhere!
2000 DP107
Equal mass
binaries
• 1 in 6 observed is binary!
• Rapidly rotating primaries!
Hermes
1994 CJ1
• Primaries roughly spheroidal!
• Circular, equatorial orbits!
2003 YT1
• Secondaries likely tidally
locked (like Earth’s Moon)
2000 CO101
1999 KW4
2000 UG11
2006 VV2
2004 DC
Binary NEA 1999 KW4
For Visualizations of the 1999 KW4 Binary Asteroid System,
Radar-Derived Shape Models, and Their Corresponding Synthetic
Radar Spectra and Radar Images, see Dr. James E. Richardson’s
(Arecibo Observatory) YouTube Channel at:!
https://www.youtube.com/user/jerichardsonjr
1998 QE2 Mutual Orbit !
and Secondary Shape
Triple Asteroid Systems
Above: 1994 CC!
Left: 2001 SN263
Radar Astronomy Summary
• Radar is a unique method of studying solid objects
from Mercury out to Saturn’s rings!
• Image resolution surpassed only by dedicated
spacecraft!
• Radar is a vital tool for impact hazard assessment!
• Efficiency compared to spacecraft allows us to
describe the asteroid population!
• Near-Earth asteroid population is heterogeneous!
• Binaries (~16%) + Contact Binaries (~14%) +
Triples (~1%) ~ one-third of NEAs!